Feasibility and benefits of laminar flow control on supersonic cruise airplanes /
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| Author / Creator: | Powell, A. G. |
|---|---|
| Imprint: | Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989] |
| Description: | 1 volume. |
| Language: | English |
| Series: | NASA contractor report ; 181817 NASA contractor report ; NASA CR-181817. |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/7732544 |
MARC
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| 035 | |a (OCoLC)384172382 | ||
| 037 | |a N 89-26841 |b NASA | ||
| 040 | |a GPO |b eng |c GPO |d GPO |d MvI | ||
| 074 | |a 0830-H-14 (online) | ||
| 086 | 0 | |a NAS 1.26:181817 | |
| 100 | 1 | |a Powell, A. G. | |
| 245 | 1 | 0 | |a Feasibility and benefits of laminar flow control on supersonic cruise airplanes / |c A.G. Powell, S. Agrawal, T. R. Lacey. |
| 264 | 1 | |a Hampton, Va. : |b National Aeronautics and Space Administration, Langley Research Center, |c [1989] | |
| 300 | |a 1 volume. | ||
| 336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
| 337 | |a computer |b c |2 rdamedia | ||
| 338 | |a online resource |b cr |2 rdacarrier |0 http://id.loc.gov/vocabulary/carriers/cr | ||
| 490 | 1 | |a NASA contractor report ; |v 181817 | |
| 538 | |a Mode of access: Internet from the NTRS web site. Address as of 06/09/09: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890017470%5F1989017470.pdf ; current access is available via PURL. | ||
| 500 | |a Title from title screen (viewed Jun. 9, 2009) | ||
| 650 | 7 | |a Aerodynamic configurations. |2 nasat | |
| 650 | 7 | |a Boundary layer control. |2 nasat | |
| 650 | 7 | |a Boundary layer stability. |2 nasat | |
| 650 | 7 | |a Feasibility analysis. |2 nasat | |
| 650 | 7 | |a Fighter aircraft. |2 nasat | |
| 650 | 7 | |a Laminar boundary layer. |2 nasat | |
| 650 | 7 | |a Laminar flow. |2 nasat | |
| 650 | 7 | |a Supersonic aircraft. |2 nasat | |
| 650 | 7 | |a Supersonic cruise aircraft research. |2 nasat | |
| 650 | 7 | |a Supersonic transports. |2 nasat | |
| 700 | 1 | |a Agrawal, Sudhir. |0 http://id.loc.gov/authorities/names/n93014783 |1 http://viaf.org/viaf/47501547 | |
| 700 | 1 | |a Lacey, T. R. | |
| 710 | 2 | |a Langley Research Center. |0 http://id.loc.gov/authorities/names/n79134855 |1 http://viaf.org/viaf/127305149 | |
| 776 | 1 | |a Powell, A. G. |t Feasibility and benefits of laminar flow control on supersonic cruise airplanes. |h 1 v. |w (OCoLC)384139602 | |
| 830 | 0 | |a NASA contractor report ; |v NASA CR-181817. | |
| 856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/LPS113610 |y Government Publishing Office |
| 903 | |a HeVa | ||
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| 928 | |t Library of Congress classification |l Online |c UC-FullText |u https://purl.fdlp.gov/GPO/LPS113610 |z Government Publishing Office |g ebooks |i 12815017 | ||